TCDS TC 2-9

MILLER, EDWARD E. MODELS: Miller Dawydoff-Cadet UT-1 (Glider), 1 PCLM T.C. NUMBER: 2-9 I - Model UT-1, 1 PCIM (Approved 11/30/43) •YpE irspeed limit: Glide or dive - 65 mph True Ind. Auto-winch tow - 45 mph True Ind. C.G. range (28.1 percent MAC) to (+17.8) (+32.5 percent MAC) Datum Wing leading edge at side of fuselage MAC 54.6 in. I.E. MAC (0) leveling means Longerons at cockpit horizontal Standard weight No. seats 1 (-4) (See NOTE 1) Baggage Control surface flevator Up 34 degrees Down 34 degrees movements Rudder Right 28 degrees Left 26 degrees Aileron Up 8 degrees Down 29 degrees Stabilizer Up 1 degree Down O degrees Serial Nos. • onli eligible Required equirment tems 401 and 40 SPECIFICATIONS PERTINENT TO ALL MODELS: Certification basis CAR 05.031 EQUIPtems included in required lists under specifications pertinent to individual models may not be removed unless replaced by approved equivalent items. The effect upon balance of all equipment changes must be computed and the aircraft operation record revised accordingly. Values in inches shown in parenthesis after each item represent horizontal arms to the C.G. of the item measured minus (-) ahead and plus (+) to the rear of the datum. A plus (+) or minus (-) sign preceding the weight of an optional item indicates the net weight change between that item and the equivalent required Interior Equipment: 401. Air speed indicator • 5 IDE - 19 402. Altimeter E 108 - 19 Miscellaneous (not listed above): 600. Miscellaneous items as noted in approved weight and balance report. NOTE (İ¡ The following placards must be installed in full view of the pilot: "Inverted flying prohibited." "Shock-cord launching prohikited." "Aircraft tow prohibited." (a) "visual-contact day flying only permitted. (2) Authorized Loadings (a) Maximum weight of pilot and parachute 170 lbs. b) Minimum weight of pilot and parachute 120 lbs.